Smallsat, Launching
DEPLOYER TECHNOLOGY.
For nanosatellites
A robust, lightweight ECSS-compliant deployer, scalable for 3 U, 6 U and 12 U while accommodating solar arrays.
Product
compatibility
- Mechanically interfaces with cubesats by means of guide rails
- Mechanically interfaces with launch vehicle by means of standard fasteners
- Electrically interfaces with launch vehicle for telemetry
- Extra volume dedicated to solar arrays for the 6 sides of the satellite
Manoeuvres
and performances
Easily modular to contain 3 U to 12 U
Provides deployment status signal
Main
Benefits
Payload
volume
Specifications
and configurations
Mass
—–
5 kg
Payload mass
—-
24 kg
Ejection velocity
—-
For a 24 kg payload (maximum mass of a 12 U): from 0.5 to 1 m/s.
This is an easily adjustable parameter.
Envelope (H x W x L)
—-
286 x 286 x 400 mm
Configuration
—-
- 12 U
- Custom size on request
- From 3 U to 12 U (3 U x 4 / 6 U x 2)
Partner
